View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 26998U 26076.20753632 +.00000000 +00000-0 +13677-3 0 00003
2 26998 74.0668 60.1869 0002961 266.1921 93.8925 14.95047456 03
| Epoch (UTC): | 17 March 2026 04:58:51 |
| Eccentricity: | 0.0002961 |
| inclination: | 74.0668° |
| perigee height: | 580 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 60.1869° |
| argument of perigee: | 266.1921° |
| revolutions per day: | 14.95047456 |
| mean anomaly at epoch: | 93.8925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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